发明名称 High bandwidth inertial measurement unit
摘要 An inertial measurement unit is disclosed which includes a system of gyros for sensing angular rates, a system of accelerometers for sensing angular accelerations, an integrator for deriving gyro-less angular rates from the sensed angular accelerations, and a complimentary filter for blending the sensed angular rates and the gyro-less angular rates to produce a virtual angular rate output for the inertial measurement unit.
申请公布号 US8020442(B2) 申请公布日期 2011.09.20
申请号 US20080154400 申请日期 2008.05.22
申请人 ROSEMOUNT AEROSPACE INC. 发明人 ELL TODD A.;RUTKIEWICZ ROBERT D.
分类号 G01P3/44 主分类号 G01P3/44
代理机构 代理人
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